CN1780982A - Rotor blade of a wind energy facility - Google Patents
Rotor blade of a wind energy facility Download PDFInfo
- Publication number
- CN1780982A CN1780982A CNA2004800114863A CN200480011486A CN1780982A CN 1780982 A CN1780982 A CN 1780982A CN A2004800114863 A CNA2004800114863 A CN A2004800114863A CN 200480011486 A CN200480011486 A CN 200480011486A CN 1780982 A CN1780982 A CN 1780982A
- Authority
- CN
- China
- Prior art keywords
- rotor blade
- wind
- power generating
- generating system
- rotor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 claims description 14
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 11
- 230000008569 process Effects 0.000 claims description 10
- 238000000926 separation method Methods 0.000 claims description 8
- 238000010248 power generation Methods 0.000 claims 2
- 239000000463 material Substances 0.000 description 22
- 238000013461 design Methods 0.000 description 12
- 230000000694 effects Effects 0.000 description 8
- 241000446313 Lamella Species 0.000 description 7
- 230000008859 change Effects 0.000 description 6
- 230000002349 favourable effect Effects 0.000 description 6
- 230000006872 improvement Effects 0.000 description 5
- 238000007789 sealing Methods 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000004590 computer program Methods 0.000 description 2
- 210000000527 greater trochanter Anatomy 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- UJCHIZDEQZMODR-BYPYZUCNSA-N (2r)-2-acetamido-3-sulfanylpropanamide Chemical compound CC(=O)N[C@@H](CS)C(N)=O UJCHIZDEQZMODR-BYPYZUCNSA-N 0.000 description 1
- 241001669680 Dormitator maculatus Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
- F03D1/0641—Rotors characterised by their aerodynamic shape of the blades of the section profile of the blades, i.e. aerofoil profile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0675—Rotors characterised by their construction elements of the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/31—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape
- F05B2240/311—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape flexible or elastic
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Abstract
The invention relates to a rotor blade of a wind energy facility and to a wind energy facility. The invention aims at providing a rotor blade with a blade profile or a wind energy facility, which has an improved efficiency. To achieve this, several solutions are possible: rotor blade of a wind energy facility, wherein the rotor blade has a position of maximum thickness of approximately 15 % to 40 %, preferably from approximately 23 % to 28 %; the biggest thickness of the profile is approximately 20 % to 45 %, preferably from about 32 % to 36 %; the rotor blade has a two part configuration in the root area; a part of a rotor blade is configured in the outer side of the hub lining; the ratio between the profile depth of a rotor blade and the diameter of the rotor is approximately from 0.04 to 0.1 and the ratio between the depth of the profile of a rotor blade and the diameter of the spinner is between 0.5 and 1.
Description
Technical field
The present invention relates to a kind of rotor blade and corresponding wind-power generating system of wind-power generating system.
Background technique
With regard to the state of relevant prior art, we have consulted the author who published in 1996 is the strange person of outstanding talent's of Airy (Erich Hau) book " wind-power generating system " (Wind power systems).This this school bag contains the example of the cross section of the rotor blade of some wind-power generating systems, wind-power generating system of prior art and rotor blade.Be presented among Fig. 5 .34 on the 102nd page of this book according to the geometrical construction size of the pneumatic profile (profile) of NACA.As shown in the drawing, rotor blade is described by following parameters: corresponding to the profile degree of depth (profile depth) of chord length; The maximum arch of the maximum height of the skeleton line of qualification string top (or arch ratio); The position of maximum arch, promptly in the cross section of rotor blade with respect to the position of the maximum arch of the profile degree of depth; Limit the largest face thickness that a center of circle is positioned at the maximum diameter of the inscribed circle on the skeleton line; And the position of maximum ga(u)ge, promptly the cross section of rotor blade presents the position of largest face thickness with respect to the profile degree of depth.In addition, the profile coordinate of leading-edge radius and upper and lower sides also is used for describing the cross section of rotor blade.Also have, the term in the strange person of outstanding talent's of Airy the book also is used for describing the cross section according to rotor blade of the present invention.
Other rotor blade of prior art is disclosed in DE 103 07 682, US 5,474,425, US6,068,446 and DE 694 15 292 in.
Can be optimized rotor blade from several different aspects.Rotor blade not only should quietly turn round, also should have a maximum power performance, to start the rotation of wind-power generating system and be issued to rated velocity in possible minimum wind force intensity when hanging down wind speed, this rated velocity promptly reaches for the first time the rotating speed of the rated power of wind-power generating system.If next wind speed increases; the general practice is to increase the rotor blade that is adjusted at the wind-power generating system of being regulated by the angle (pitch) that facings the wind in the wind; make the surface area that facings the wind that when keeping rated power, reduces rotor blade, with protection whole wind force generating system with and parts be not subjected to mechanical failure.Under any circumstance, the aerodynamic characteristic of the blade profile of the rotor blade of a wind-power generating system is most important.
Summary of the invention
The objective of the invention is to disclose a kind of rotor blade and a kind of corresponding wind-power generating system with rotor blade profile, it is compared and can raise the efficiency with the rotor blade up to now.
According to the present invention, described purpose is realized by the rotor blade that has according to a rotor blade profile of the feature of independent claims.Other favourable improvement is limited by dependent claims.
Concrete coordinate according to rotor blade profile of the present invention is listed in the table 1.
Description of drawings
Present invention is described below with reference to a few width of cloth accompanying drawings, and each figure shows:
Fig. 1 is the front elevation according to a wind-power generating system of the present invention;
Fig. 2 is the rear view according to a wind-power generating system of the present invention;
Fig. 3 is the side view according to a wind-power generating system of the present invention;
Fig. 4-8 is the view according to the different direction of rotor blade of the present invention;
Fig. 9 is the zoomed-in view according to a wind-power generating system of the present invention;
Figure 10 is according to a rotor blade view of the present invention;
Figure 11-17,19 is the different views according to wind-power generating system of the present invention; And
Figure 18 is according to the cross section of a rotor blade of the present invention (near the zone of wheel hub).
Embodiment
Particularly, the profile of rotor blade of the present invention is arranged in the zone at rotor blade adjacent rotor blade installation portion (position that connects wheel hub).Preferably, the described profile of the application be positioned at rotor blade with respect to self whole length first three/place.The rated power that depends on wind-power generating system, the total length of these rotor blades between 10m between the 70m.For example, the rated power of the wind-power generating system of an Enercon-112 type (the about 112m of diameter) is 4.5MW, and the rated power of the wind-power generating system of an Enercon-30 type is 300kW.
Feature according to a uniqueness of the profile of rotor blade of the present invention is the 25-40% that its largest face thickness is approximately this rotor blade chord length, is preferably 32-36%.In Figure 18, this largest face thickness is 34.6% of a rotor blade chord length.String 1 shown in Figure 1 extends to the end points 4 of rotor blade taper 5 from the center 2 of the trailing edge 3 of rotor blade.The position of maximum ga(u)ge promptly with respect to the position of the largest face thickness of length of blade, approximately is positioned at the 20-30% place of chord length, is preferably 23-28%.In an illustrated embodiment, the position of maximum ga(u)ge is 25.9%.This maximum ga(u)ge is determined perpendicular to described string, and this maximum position is for the rotor blade taper.
Figure 18 has also shown a so-called skeleton line 7.This skeleton line has all been determined a half thickness of rotor blade 8 at an arbitrary position.Therefore, this skeleton line is not straight, but just in time rotor blade 7 on the pressure side 9 and the suction side 10 of rotor blade 7 on corresponding point between.This skeleton line intersects at rotor blade trailing edge and rotor blade taper and string.
Approximately be positioned at the 55-70% place of chord length in position, be preferably 59-63% according to the maximum arch in the cross section of rotor blade of the present invention.The position of maximum arch in an illustrated embodiment approximately is positioned at 61.9% place.Maximum arch is approximately the 4-8% of chord length in this case, is preferably the 5-7% of chord length.In an illustrated embodiment, maximum arch is approximately 5.87% of chord length.
Another tangible unique property according to the profile of rotor blade of the present invention is, on the pressure side " the intersecting " twice with described string of this rotor blade.Therefore, this profile on the pressure side forms recessed in this zone, and on the pressure side forms protrusion in the front portion of profile.In recessed district on the pressure side, suction side is by one in the corresponding opposed area on this suction side straight basically line restriction.
As everyone knows, also can will on the pressure side form recessed arch, or suction side is formed a straight flange.But the combination of these two kinds of methods especially, is most important to rotor blade profile according to the present invention, and is the feature of rotor blade profile of the present invention.
Shown in the rotor blade trailing edge of profile also be thick especially.But this can not cause at the trailing edge of rotor blade and produce noise because shown in profile be arranged on the circle that limits by the rotor blade taper interior 1/3rd in, and the path velocity that should locate neither be very high.
The x-y coordinate of profile shown in the drawings is listed in the table 1, and these coordinates have accurately been described the profile of rotor blade of the present invention.
The aerodynamic configuration of rotor blade can improve by such design rotor blade root zone: rotor blade has maximum ga(u)ge in this zone, and therefore, this rotor blade is approximately more or less and optimum pneumatic profile similarly trapezoidal (plane view).At root area, this rotor blade is preferred to be realized like this: will repack at least one angular coordinates place consistent with the exterior contour in this cabin towards the rotor blade butt in wind-power generating system cabin, for example, when rotor blade is positioned at its position corresponding with design wind speed, between the exterior contour in the rotor blade butt of wind-power generating system and this cabin, there is being a width to be approximately the space of 5mm to 10mm.
A kind of rotor blade with aforementioned feature shows in some cases can significantly increase power, promptly up to 10% power.Because this unexpected power increases, wind-power generating system according to the present invention increases in the output power that is lower than under the arbitrary given wind speed of rated wind speed.In addition, this wind-power generating system and the former rated power that can comparatively fast reach it of comparing.This means that this rotor blade also can earlier rotate (adjust facing the wind angle) to reduce to sound and to act on mechanical stress in this system.
The present invention is based on following thought, nowadays the conventional rotors blade shape of Shi Yonging is with different wind speed but test under uniform airflow in wind-tunnel.But natural wind blows seldom equably and follows the random distribution rule, and fitful wind may cause that air-flow separates on traditional rotor blade, particularly blade not by pneumatic processing and form in the mode of the best, near the intravane region of rotor hub.Air-flow continues to separate on the certain distance of the direction of rotor blade zone (rotor blade taper) outside.This may cause the airflow breakaway in the zone of an air bubble-shaped and cause energy loss.Because rotor blade has been carried out clean design (clean design), the present invention can also significantly increase energy at the internal rotor leaf area of the above-mentioned type.
If use a profile of standard traditionally, and the profile of determining with experience of not using the application and being proposed, the pneumatic clean design of rotor blade may approximately double (it is corresponding to the chord length of rotor blade) in the profile degree of depth of rotor blade lower area (near the zone of wheel hub).But, need the remarkable profile thickness of front area to transmit a safe load and obtain one greater than 2 lift coefficient C
A
The rotor blade of prior art is fabricated to usually can realize maximum flow ground saving material in described inner region.The exemplary of the rotor blade of this prior art is presented at the author that published in above-mentioned 1996 on the 114th and 115 page of the strange person of outstanding talent's of Airy book " wind-power generating system ".According to these examples, the maximum profile degree of depth always is positioned at apart from rotor blade assembly department a distance, promptly near the rotor blade mounting zone, wherein can save material according to prior art in this zone.But when using one in plane view during similar trapezoidal optimised shape, the Extreme breadth of rotor blade is not positioned at apart from rotor blade assembly department a distance, and just in time is positioned at the zone of rotor blade assembly department itself.Therefore, can not save material on the inner region maximum flow ground of this rotor blade here.
Saving the reason of material can see in the static state consideration to flow conditions when (above-mentioned) calculating/exploitation rotor blade.In addition, the program of popular calculating rotor blade is divided into rotor blade plurality of single section and calculates each rotor blade section separately to draw the evaluation to whole rotor blade.
But full-scale condition is very different.The first, wind can not blow in the certain surface area evenlyly and permanently, but is rendered as a kind of tangible random behavior.The second, wind speed is a key factor, because the outer circular velocity of rotor blade is very low in inner region (being the rotor hub near zone), makes the change of the angle of attack highly depend on instantaneous value in this zone.Therefore, boundary layer separation also occurs in the inner region of rotor blade with a correspondent frequency.
Hysteresis is effective under these circumstances.In case wind speed drops to former wind speed, for example after a gust of wind, the boundary layer on the rotor blade can not recovered immediately, but wind speed must further reduce earlier (promptly needing further to adjust the angle of attack) till recover in the boundary layer on the rotor blade.But, if wind speed does not further reduce, being likely how the incoming flow wind speed all has certain power to be applied on the rotor blade in a longer-term, reason is that the boundary layer on this rotor blade surface also there is not recovery.
The rotor blade of design has significantly reduced the risk of boundary layer separation according to the present invention.Described thicker type face also helps to reduce the risk of separation.The Another reason that efficient enlarges markedly is, in case after the boundary layer separation, the output power that described hysteresis effect causes reduces and will continue one period long period (when using the rotor blade of prior art).
The partly cause that described efficient increases is that also wind has utilized the path of minimum drag.The very thin design of the inner region of the close wheel hub of rotor blade (significantly economical with materials) be equivalent to the rotor circle obtain one " small opening (slip hole) " in the district by what described rotor blade skimmed over, thereby air-flow tends to flow through this small opening.This be popular computer program another weakness sign---the calculating of these programs is always based on the even distribution on the border circular areas that is skimmed over by rotor blade.
If by in the design of using a trapezoidal rotor blade near hub area and should " small opening " sealing, the distribution of the air-flow on whole border circular areas improves and the effect of rotor blade exterior domain obtains some reinforcements so.The result is that the sealing of this " small opening " has improved the power factor according to rotor blade of the present invention.
This has also pointed out another weakness of popular computer program, because these programs also will be considered to a rotor blade section that plays a role fully with the rotor blade section that " small opening " directly adjoins.But (frequent boundary layer separation the back takes place followed by the recovery that is required flox condition) is true really not so because described special flox condition.
Figure 11-17 shows a front elevation and a side view according to wind-power generating system of the present invention respectively.In these figure, described three rotor blades carry out the transition to the outer contour in cabin basically seamlessly in the zone near wheel hub.But this only is only applicable to the position with the specified corresponding rotor blade in wind position.
In case the increase of wind-force exceeds specified wind-force value, conventional method is to adjust at leisure with the wind rotor blade by becoming the angle that facings the wind (the angle adjustment of facining the wind).Wherein, Figure 15 shows that this is easy to cause forming the gap of big width within it between regional lower edge of rotor blade and cabin.But Fig. 4 shows that also the outside in cabin comprises a cross section to a great extent corresponding to the structure of rotor blade near the profile of hub area.When rotor blade was adjusted to a corresponding angle of attack, this structure was located immediately at below the rotor blade of rated velocity running, makes this structure and rotor blade only form a narrow gap near between the zone of wheel hub.
Therefore, the outer contour in cabin also comprises the section of a rotor blade that does not form as one with rotor blade.
In rotor blade profile shown in Figure 180, the taper radius is approximately 0.146 of the profile degree of depth.
According to Figure 18, suction side comprises long basic straight zone that is.For example, this zone is as described below: between the profile degree of depth 38% and 100% between the zone, described radius equals 1.19 times of length of the profile degree of depth.Between the profile degree of depth (seeing Figure 18) 40% and 85% between this zone, described radius equals 2.44 times of the profile degree of depth.Between the profile degree of depth 42% and 45% between this zone, described radius equals 5.56 times of the profile degree of depth.
Between the profile degree of depth 36% and 100% between this zone, be approximately 0.012 of the profile degree of depth with the maximum value of the deviation of a desirable straight line.This value is determined, does not define because radius of curvature is not a maximum curvature radius constant and that each is regional.
In the example shown, the length of suction side is approximately 1.124 times of the profile degree of depth, and length on the pressure side is approximately 1.112 times of the profile degree of depth.This means that suction side only is longer than on the pressure side a little.Therefore, if the length of suction side and on the pressure side length are than less than 1.2, preferably less than 1.1 or be very favorable between 1 and 1.03.
These figure show that the profile degree of depth of rotor blade is at cowling, and---being the outside, cabin of wind-power generating system---locates maximum.In the diameter of a rotor was 30 meters wind-power generating system, the profile degree of depth at the cowling place can be for example about 1.8 to 1.9 meters, to be preferably 1.84 meters.If the diameter of cowling is approximately 3.2 meters, rotor blade is approximately 0.575 at the profile degree of depth and the cowling diameter ratio at cowling place.Therefore, if the profile degree of depth and cowling diameter ratio greater than 0.4 or be very favorable between 0.5 and 1.In this, can choose any value in the above-mentioned interval.In above-mentioned example, the profile degree of depth is approximately 0.061 with the ratio of root diameter.Clearly, if the ratio of the profile degree of depth and root diameter is greater than a value of [sic] between 0.05 and 0.01---the example value of getting is very favorable for the efficient of rotor blade in such cases, " small opening " minimum that is caused.
In another example, first three of rotor blade/one profile cross section is shown among Figure 18, and the profile degree of depth at cowling place approximates 4.35 meters greatly among this figure, and the overall diameter that the diameter of cowling is approximately 5.4 meters and rotor is 71 meters.In this case, the profile degree of depth and cowling diameter ratio be 0.806 and the ratio of the profile degree of depth and root diameter still be 0.061.Above-mentioned value is for three vane rotors with down with the wind angle adjustment.
As mentioned above, the widest position of rotor (the maximum profile degree of depth place of this rotor) can be formed directly in the blade installation portion zone.Term blade installation portion be meant blade connect (in conjunction with, be spirally connected etc.) to the zone of the wheel hub of wind-power generating system.In addition, the downside of rotor blade promptly towards that side in the cabin of wind-power generating system, forms or consistent with vertical external frame in cabin to a great extent.Therefore, one is in the facing the wind rotor blade of position, angle (feathered pitch position) (in fact not having the surface also to aim at wind direction) of feathering and is parallel to lower edge towards the cabin, and the distance between the outer contour in this lower edge and cabin is minimum, preferably less than 50cm, in fact less than 20cm.
If this moment, this rotor blade was adjusted in the wind field, its maximum surface also is positioned at the inner region (small opening is very little) of rotor blade.The strange person of outstanding talent's of the Airy of quoting previously book shows that the rotor blade of prior art continues to reduce (rotor blade is narrow at their the wideest point at this place's ratio) in the zone near wheel hub.On the contrary, be positioned at zone particularly, make the potential energy of wind to be utilized fully in this position near wheel hub according to the wideest point of rotor blade of the present invention.
Many known, particularly very big rotor blade is very wide at the rotor blade in the zone of close wheel hub.This rotor blade can also by two-part form so that transport such rotor blade (the greater trochanter blade, for example, length surpasses the rotor blade of 30m, its near the width of hub area preferably between 5m between the 8m).Described two-part separate in transportation process and can assemble this rotor blade after this rotor blade arrive the mounting point.These two-part for example interconnected by screw connection or inseparable connection (welding) when this rotor blade was installed on the wind-power generating system.Particularly for the greater trochanter blade, this is not any problem, because the inside of such rotor blade also gets in assembly process.The outside of this rotor blade has uniform outer appearance and the separation line between two parts of finishing assembling and is difficult to visible or cannot see fully.
Preliminary measurement result shows, compares with existing conventional rotors blade, and the rotor blade of design can significantly improve efficient according to the present invention.
According to Fig. 1-17, realize the rotor blade of a kind of wind-power generating system of the present invention, make their the maximum profile degree of depth be positioned at the zone of close wheel hub, and this rotor blade extend to the position of the cabin fair water cone (cowling) of the power compartment that is close to this wind-power generating system along the whole profile in the wheel hub near zone.This causes at least adjusting to up to the position of the corresponding angle of wind speed of rated wind speed scope the time at rotor blade, and the gap between rotor blade and the cabin fair water cone is very little.For example, in Fig. 1,2 and 3, rotor blade also extends to a cabin fair water cone and a contiguous position of profile depth areas, back.Shown in another variant in, for example in Figure 11-17, the outside of cabin fair water cone itself has a rotor blade section 30, but this section does not form the part of whole rotor.Figure 15 and 17 shown especially, and the described rotor blade portion that is formed on nacelle exterior is fixed on this position, and its angle to be arranged to up to rated wind speed the time position, angle of rotor blade corresponding.This means at least at wind speed during, in the gap that also forms a minimum behind the downside of rotor blade and the cabin between the profile depth areas up to rated wind speed.
The rotor blade that Figure 19 has also clearly illustrated the design according to the present invention has very little " small opening " that is used for wind in rotor center.
Figure 18 has shown the cross section of rotor blade according to the present invention along the A-A line among Figure 17, and promptly rotor blade is in the profile of wheel hub near zone.
Figure 17 also comprises a sign that shows the diameter D of cowling.
The diameter of rotor is described by the radius of its inswept border circular areas in the rotor rotation process.
According to Figure 15 and other figure, the part 30 of rotor blade does not form the part of described rotor blade, but forms the part of fair water cone outside, cabin.This appropriate section can be installed to described cabin or one is connected or welded to the cabin with screw.
Very big according to the length of the application's rotor blade and under the corresponding rotor blade degree of depth of the wheel hub near zone very big situation that---is chord of blade---, this zone is feasible with blade separated into two parts or many parts with the transportation of simplifying rotor blade.In this case, rotor blade was not ressembled this rotor blade before reaching the mounting point that whole rotor blade is installed to wheel hub.Under these circumstances, the part rotor blade can be realized as shown in figure 20.According to this figure, lack one section in the trailing edge zone.The section of lacking can be recovered profile shown in Figure 180 in this zone by enclosing.
Described two-part can interconnect by screw, welding or other fixation method.
Also can be provided in the device of surface size of described this rotor blade of area change of rotor blade.Corresponding variant must be noted that shown in Figure 21-23 it is schematic (profile of rotor blade is substantially corresponding to profile shown in Figure 180) that the cross section of the rotor blade shown in these figure should be understood to.
Variant shown in Figure 21-23 provides the advantage that can reduce the whole surface of rotor blade as needs.This is under the extreme wind condition and be very actual in the transportation process at rotor blade, because its allows or simplifies the transportation of rotor blade at least and prevent the overload of wind-power generating system under extreme wind condition.
In a particularly preferred variant of the present invention, part surface is made up of a deformable material, and this material has formed the part of a closed container (this container forms back profile shell).This closed container can be equipped with the gas medium that for example is subjected to certain pressure.This has caused this rotor blade to have a part of expandable surface, and therefore the gas that it can be extracted out in transportation process or under extreme wind condition in this blade need still less space, and can surrender under the effect of blast.This has reduced the effective surface area and the windward side of rotor blade.Comprise that the load on the components downstream of control tower has also reduced simultaneously.
In another variant of the present invention, rotor blade comprises second wing structure in box body (rear box) (not showing) zone, described back in Figure 20, this wing structure on this zone and/or in can move.Described deformable material can be fixed on a precalculated position of this second wing structure, and a side of this deformable material can be installed on the rotatable winder unit.
Described second wing structure can wind-power generating system normal manipulation mode stretch, promptly extending arm full extension or telescopic boom extend fully.One side of described deformable material is installed on the rotatable winder unit.If the surface area of rotor blade surface must reduce, then rotate this winder unit---being similar to a rain cover---to roll described deformable material.Folding arm is folding simultaneously and reduce second wing structure in the size that can reduce surface area, makes the surface area of rotor blade correspondingly reduce.
In an optional variant of the present invention, the part of rotor blade surface comprises and is separately positioned on a sheet type band on the supporting guide, and this supporting guide can pivot around its longitudinal axis.In normal manipulation mode, these sheet type bands are arranged in a row and make them increase the pneumatic effective surface area of rotor blade.Therefore and the corresponding surface area that reduces rotor blade in the rotor blade transportation process or under the extreme loads effect, described supporting guide can pivot, and makes corresponding thin slice move on to the lee face of for example remaining rotor blade, and.
In a particularly preferred further improvement of the present invention, the moveable part of described pneumatic effective rotor blade surface can be formed at the independent flat unit of the direction superior displacement of the rotor blade degree of depth by one.Under normal operation mode, this flat unit preferably increases the surface area of rotor blade in suction side, to produce a big pneumatic effective surface area.
In order to reduce surface area, the system of flaps that this flat unit can be similar to a wing moves this flat unit, makes it to move on in the rotor blade and by the remaining surface coverage of rotor blade, or moves on on the rotor blade and cover the surface of rotor blade.Under any circumstance, this causes long-pending the reducing of rotor blade surface.
In an optional variant of the present invention, a side of this flat unit pivotally is connected to first wing structure or rotor blade trailing edge.The surface area of rotor blade can by with this unit around this unit shaft towards the suction side of rotor blade or on the pressure side pivot and change.
If this flat unit has pivoted about 90 °, it is positioned on the rotor blade perpendicular to airflow direction substantially and produces a corresponding retarding efffect, because it hinders the Surface runoff of air along rotor blade.
Hereinafter with reference to accompanying drawing several variants of the present invention are described in detail.They show:
Figure 20 is the plan view according to a rotor blade of the present invention;
Figure 21 is the plan view according to the leading portion of a rotor blade of the present invention;
Figure 22 is the schematic cross-sectional according to first variant of a rotor blade of the present invention;
Figure 23 is the schematic cross-sectional according to second variant of a rotor blade of the present invention;
Figure 24 a, 24b are the schematic cross-sectional according to the 3rd variant of a rotor blade of the present invention;
Figure 25 is the schematic cross-sectional according to the 4th variant of a rotor blade of the present invention;
Figure 26 is the schematic cross-sectional according to the 5th variant of a rotor blade of the present invention;
Figure 27 a and 27b are the simplification cross section according to the 6th variant of a rotor blade of the present invention;
Figure 28 is the plan view according to a favourable variant of a rotor blade of the present invention;
Figure 29-33 is other favourable example of the present invention.
Figure 20 has shown a diagrammatic top view according to complete rotor blade of the present invention.Rotor blade 100 separated into two parts.With regard to its critical component, rotor blade 100 is pressed the traditional approach design.But, in the zone of closing on rotor blade root 120, promptly have that zone of the maximum blade degree of depth, can see the zone that a division is come out.The zone 140 that this zone of dividing out is a rotor blade, this regional surface area can reduce if desired, makes it no longer to be subjected to wind action.
Figure 21 has shown the rigid element of rotor blade 100, and the surface area of this part remains unchanged.This figure clearly illustrates that the pneumatic effective surface area of rotor blade 100 has reduced significantly, and the feasible particularly load under extreme wind-force situation is significantly less than the load of the rotor blade of a traditional design.
Figure 22 has shown the schematic cross-sectional of first variant of the present invention.In this case, rotor blade 100 is divided into a front area 110 and a rear portion box body (rear box) 140.This rear portion box body 140 is made up of two deformable material bands 180, and described band has formed the container 160 of a sealing with the rear wall of front area 110.If this closed container 160 now is full of the gas medium of a compression, the part that described deformable material 180 forms according to the surface area of rotor blade 100 of the present invention, this part are pneumatic effectively (and being identified by drawing reference numeral 140 in Figure 20) under normal operation mode.
This of rotor blade section can be such stability form, make that its normal effect becomes clearly under the normal wind condition.But this a part of blast that is applied to rotor blade is higher under extreme wind condition, make external pressure be higher than interior pressure, thereby rotor blade is finally externally surrendered in this case under the blast effect at rear portion box body 140 region deformations and this rotor blade.This has not only reduced the windward side under extreme wind-force, and reduces the load on the downstream configurations.
It shall yet further be noted that when for example when wind speed surpasses a predetermined value, can initiatively the medium in this part (filled media wherein is housed) of rear portion box body be extracted out to reduce the surface area of this rotor blade.This active is extracted provides such advantage: the shape of rotor blade determines forever, and if described rear portion box body may cause uncertain situation when surrendering under external pressure.
Impaired in order to prevent container 160, can for example provide a permission will be formed on the pressure relief valve (not shown) that the excess pressure in the container 160 discharges.
The required pressure of normal operation mode can utilize a compressor 170 to recover.If provide control valve and/or pressure transducer (not shown), when having fluctuation, blast also can adjust pressure in the container 160 to keep optimum operating condition always.
Figure 23 has shown second variant of the present invention, and wherein the surface of rotor blade suction side is extended rather than used a complete rear portion box body 140.This extends by a flat unit 240 that connects front area 110 forms.
This flat unit 240 can by the direction superior displacement shown in the arrow to reduce pneumatic effective surface area.This displacement can hydraulically realize by for example corresponding oil hydraulic cylinder, pneumatically realized or by realizations such as electric drive systems by pneumatic cylinder.Certainly, must be provided for corresponding pump, compressor or the drive unit (actuator) (but for the purpose of clearer, not showing these devices in the drawings) of this purpose.
Described flat unit can the shift-in front area, makes the surface coverage flat unit 240 of front area 110.Alternatively, this flat unit also can move on on the surface of front area 110, makes this flat unit 240 cover the appropriate section of front area 110.Under two kinds of situations, the pneumatic effective surface area of rotor blade 100 has all reduced.
Figure 24 a and 24b have shown the 3rd variant of the present invention.Figure 24 a shows the spool 200 of a deformable material, and label 300 has identified the folding arm that is in folded state.The method that this mechanism can be similar to a sunshade realizes.
Figure 24 b shows this variant that is under the normal operation mode.The deformable material 180 that folding arm 300 is stretched out and is mounted thereon launches from spool 200 in the process that folding arm is stretched out.Therefore, spool 200 no longer carries whole winding material.
In deployed condition, an end of deformable material 180 is fixed on the spool 200, and the other end is fixed on the end of folding arm 300 on the right of pointing in the drawings.The two ends of folding arm can be connected on the web that does not show, with the rigidity that increases described structure with the deformable material fix in position.
In order to prevent that deformable material 180 from becoming lax between the outer end of spool 210 and folding arm 300, can adorn a device (not shown) that is similar to adjustable integral lattice grid below deformable material 180, this grid is by the deformable material 180 under actuating synchronously of folding arm 300 and the support extended state.
Described process can be reduced effective surface area conversely; Folding arm 300 and described adjustable integral lattice grid (not shown) are folded also makes deformable material 300 be wrapped on the scroll core 210 simultaneously.This finally forms the spool 200 shown in Figure 24 a, and causes the effective surface area of rotor blade 100 to reduce.
In the 4th variant of the present invention as shown in figure 25, flat unit 240 pivotally is connected to front area 110 rear portions, makes it form an extension part of the suction side of front area 110.
In this case, flat unit 240 is supported by the pressure spring between the supporting structure that is arranged on flat unit 240 and front area 110 280.
Under normal operation mode, pressure spring 280 supports described flat unit 240 to make it to keep in position like this.If a unusual blast is applied to the upside of rotor blade 100, being applied to the lip-deep pressure of flat unit 240 increases, and the power that overcomes spring 280 makes flat unit shown in Figure 25 240 to pressing down, and surrenders under the blast effect.This causes the corresponding of pneumatic effective surface area to reduce.
Except using a spring 280, also can provide corresponding telescopic unit, for example hydraulic pressure or pneumatic or mechanical device are with the described flat unit of active adjustment.Also can for example utilize screw rod or worm drive device to wait remains on flat unit 240 first precalculated position or this flat unit is moved on to second precalculated position.Certainly, must provide corresponding pump, compressor or drive unit to operate these actuators, these devices are for clarity sake not shown in the drawings.
Also can determine to be applied to the wind load on the flat unit 240 in this case, wherein flat unit 240 as a function of measured wind load around said pivot, to adjust described flat unit best according to instantaneous operation conditions.
Figure 26 has shown the 5th variant of the present invention.In this 5th variant, flat unit 240 pivotally is not connected to the rear side of front area 110, and be arranged on can one can be on the swivel pin of self longitudinal axis rotation.In position shown in Figure 26, flat unit 240 forms an extension of the pneumatic effective surface area of rotor blade 100.
In order to reduce this surface area, the swivel pin 220 that is fixed with flat unit 240 on it is around its longitudinal axis rotation, the outer end that makes flat unit 240 along by shown in one of the both direction of double-head arrow sign move.This also causes the pneumatic effective surface area of rotor blade 100 to reduce, and the wind load that therefore causes being applied on all components downstream of rotor blade 100 and wind-power generating system changes.
Figure 27 a and 27b show a kind of improvement of embodiment shown in Figure 26.Flat unit by label 240 signs in Figure 26 is divided into three lamella unit 260 in Figure 27 a.Have a mind to be arranged to be separated from each other so that to be described this cutting apart in Figure 27 in these lamella unit.Certainly, them are arranged in these three unit in fact can form a surface of sealing haply, and this closing surface carries out the transition to the front area of rotor blade 100 as far as possible smoothly.
Each lamella 260 is arranged on the swivel pin of self.Each swivel pin 280 can be around the longitudinal axis rotation of self, thereby by rotate pivot each lamella 260 of swivel pin 280 around the longitudinal axis.
Figure 27 b has shown that a device according to the present invention is in following situation: wherein these lamellas are pivoted to such position, and it has reduced the pneumatic effective surface area of rotor blade 100.In this case, lamella 260 is pivoted to the lee face of front area 110.Therefore, lamella no longer forms the part on the surface of rotor blade, makes them no longer be subjected to the effect of the load of wind and any rising.
A kind of like this device is embodied as, except swivel pin 280 around their longitudinal axis rotation, distance between the left swivel pin 280 among the figure and the front area 110 of rotor blade 100 and the phase mutual edge distance between the swivel pin 280 have reduced.
Though only shown an extension part that is positioned at the suction side surface among the figure, naturally, also can be alternatively or side by side change the size on surface on the pressure side.
If a wind-power generating system has above-mentioned rotor blade, and when an extreme wind condition having occurred, not only can determine high wind-force, can also significantly reduce the size of rotor blade surface by the control corresponding device by wind-speed indicator.According to Figure 20 and 21, the surface area of the rotor blade that the surface area ratio of rotor blade shown in Figure 20 is shown in Figure 21 is big by 10%.When wind-power generating system operated in normal mode, for example, wind speed was between 2-20m/s the time, and rotor blade is adjusted to its normal size.Be higher than 20m/s in case wind speed increases to, this surface area can reduce as shown in figure 21 significantly.
Preferably, described control gear is realized in computer assisted mode, and is guaranteed can adjust respectively if desired the optimum surface area of rotor blade.
Figure 33 has shown another variant according to rotor blade of the present invention.Under this situation, described structure is made up of pivotable ring 320, and this ring 320 is covered and pivoted by a deformable films and is supported on the strong point 340 places.In the mobile process of rotor blade taper (arrow), these rings for example pivot around the described strong point 340, to change the profile of rear portion box body.
Figure 28-33 has shown other optional and additional variant of Figure 22-27b.
Figure 30 b (Figure 30 a corresponds essentially to Figure 25) has shown a kind of improvement to Figure 25, and it has an auxiliary unit 250 on the pressure side.Because the point of contact of spring 280 does not change with respect to Figure 25 and 30a respectively, unit 240 and 250 must be connected on the trailing edge, make them to pivot around a binding site 260.In some cases, can in this variant, rotor blade box body 110 be embodied as along overlapping with unit 250 on the length direction of rotor blade.
Figure 31 b (for the expansion variant of Figure 26 and 31a) also shows and is positioned at a unit 250 of on the pressure side going up, and this unit is connected on the identical axostylus axostyle 120 of suction side by a mechanical fastener as unit 240.
Figure 32 a and 32b have shown the further improvement according to the variant of Figure 27 a and 27b.The axostylus axostyle 280 of separation is provided for corresponding units on the pressure side in this embodiment.Be similar to Figure 27 a, Figure 32 a has shown a rotor blade that is under the normal operation mode.Figure 32 b has shown a kind of situation, and wherein said rear portion box body is by correspondingly rotation or mobile axostylus axostyle 280 become invalid.
Claims (19)
1. the rotor blade of a wind-power generating system, wherein the position of the maximum ga(u)ge of this rotor blade is approximately between 15% and 40%, preferably between 23% and 28%, wherein largest face thickness is roughly between 20% and 45%, preferably between 32% and 36%, and this rotor blade preferably is made up of two-part.
2. rotor blade as claimed in claim 1 is characterized in that, the cross section of this rotor blade is described by a skeleton line, and the maximum arch of this skeleton line is between 50 ° and 70 °, preferably between 60 ° and 65 °.
3. rotor blade as claimed in claim 2 is characterized in that, described maximum arch is approximately 3% to 10%, preferably approximately is 4% to 7%.
4. each described rotor blade in the claim as described above is characterized in that described cross section is preferably formed in following 1/3rd zones of this rotor blade that adjoins the rotor blade assembly department.
5. each described rotor blade of claim as described above, it is characterized in that, this rotor blade have one on the pressure side with a suction side, wherein saidly on the pressure side comprise a part, and one almost is that straight part is formed on the described suction side with recessed arch.
6. the wind-power generating system that has at least one rotor blade, this at least one rotor blade connects same wheel hub fair water cone and is installed on the rotor hub together, it is characterized in that, the part of rotor blade is formed on the outside of this wheel hub fair water cone, and be rigidly connected on this wheel hub fair water cone, wherein this part of rotor blade is not formed integrally as the part of the rotor blade of this wind-power generating system.
7. wind-power generating system as claimed in claim 6 is characterized in that, the profile that is formed on the rotor blade on the wheel hub fair water cone is substantially corresponding to the profile of rotor blade at the wheel hub near zone.
8. wind-power generating system as claimed in claim 7, it is characterized in that, this part that is formed on the rotor blade on the wheel hub fair water cone is fixed and puts in place, and arrange in the following manner substantially: when wind speed is lower than rated wind speed, and when this rotor blade was adjusted to the position that meets rated wind speed, it was located immediately near the below in the rotor blade zone the wheel hub.
9. wind-power generating system, it has at least one each described rotor blade in the claim as described above.
10. wind-power generating system particularly as claimed in claim 9, wherein, this wind-power generating system comprises a rotor with at least one rotor blade, the maximum profile degree of depth of this rotor blade is positioned at the rotor blade hub zone, the ratio of the wherein said profile degree of depth and root diameter is got a value between about 0.04 and 0.1, preferably between 0.055 and 0.7, for example, 0.061.
11. particularly as claim 9 or 10 described wind-power generating systems, this power generation system has a power compartment, it holds motor and a rotor that is connected to motor, wherein, described rotor comprises at least two rotor blades, this rotor comprises a wheel hub with fair water cone (cowling), and the diameter ratio of the profile degree of depth of rotor blade and cowling is greater than 0.4, preferably between 0.5 and 1.
12. each described wind-power generating system of claim as described above particularly, this power generation system has a rotor that preferably includes an above rotor blade, wherein, how many being shaped as of this rotor blade is similar to the trapezoidal of optimum pneumatic shape, the Extreme breadth of this rotor blade is positioned at the root area of rotor blade, and forms consistent with the outer contour (vertically) in cabin substantially towards the rotor blade root edge in wind-power generating system cabin.
13. wind-power generating system as claimed in claim 12 is characterized in that, when described rotor blade forwarded feathering to and facings the wind the position, angle, the rotor blade lower edge towards the cabin almost was parallel to the cabin outer contour at root area.
14. wind-power generating system as claimed in claim 13 is characterized in that, in the described feathering position, angle that facings the wind, towards the rotor blade lower edge in cabin and the distance between the outer contour of cabin less than 50cm, preferably less than 20cm.
15. each described wind-power generating system of claim is characterized in that as described above, described rotor blade tilts to depart from the principal plane of rotor blade at root area.
16. each described wind-power generating system of claim is characterized in that described rotor blade forms two-part at root area as described above, wherein, separation line is vertical towards this rotor blade.
17. wind-power generating system as claimed in claim 16 is characterized in that, be installed to described rotor blade in the wind-power generating system after, just assemble described two-part of this rotor blade.
18., it is characterized in that two-part of described rotor blade keep separately as claim 16 and 17 described wind-power generating systems in transportation process.
19. each described wind-power generating system of claim as described above particularly, it is characterized in that, this wind-power generating system comprises at least one rotor blade, this rotor blade has a suction side and one on the pressure side, wherein the length of suction side and length ratio on the pressure side are less than 1.2, preferably less than 1.1, particularly between 1 and 1.03.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10319246.8 | 2003-04-28 | ||
DE10319246A DE10319246A1 (en) | 2003-04-28 | 2003-04-28 | Rotor blade of a wind turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1780982A true CN1780982A (en) | 2006-05-31 |
CN100366893C CN100366893C (en) | 2008-02-06 |
Family
ID=33393962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB2004800114863A Expired - Fee Related CN100366893C (en) | 2003-04-28 | 2004-03-29 | Rotor blade of a wind energy facility |
Country Status (17)
Country | Link |
---|---|
US (1) | US7946803B2 (en) |
EP (2) | EP1620646B1 (en) |
JP (2) | JP4504971B2 (en) |
KR (1) | KR100812796B1 (en) |
CN (1) | CN100366893C (en) |
AR (1) | AR046912A1 (en) |
AU (1) | AU2004234487B2 (en) |
BR (1) | BRPI0409782B1 (en) |
CA (2) | CA2524208C (en) |
DE (1) | DE10319246A1 (en) |
DK (1) | DK1620646T3 (en) |
ES (1) | ES2778830T3 (en) |
NO (1) | NO20055599L (en) |
NZ (1) | NZ543574A (en) |
PT (1) | PT1620646T (en) |
WO (1) | WO2004097215A1 (en) |
ZA (1) | ZA200508323B (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102003333A (en) * | 2010-12-21 | 2011-04-06 | 中国科学院工程热物理研究所 | Wind turbine blade with de-noising function |
CN102192079A (en) * | 2010-03-18 | 2011-09-21 | 诺德克斯能源有限公司 | Wind turbine rotor blade |
CN102192109A (en) * | 2010-03-18 | 2011-09-21 | 诺德克斯能源有限公司 | Wind turbine rotor blade |
CN102407779A (en) * | 2010-09-21 | 2012-04-11 | 周鹏 | Power generation device for power motor vehicle |
CN103244359A (en) * | 2013-05-30 | 2013-08-14 | 国电联合动力技术有限公司 | Moderate-thickness airfoil blade of large-scale fan |
CN103321857A (en) * | 2013-07-08 | 2013-09-25 | 国电联合动力技术有限公司 | Large-thickness blunt-trailing-edge airfoil-shaped blade of large-scale wind turbine |
CN101749188B (en) * | 2008-12-03 | 2014-01-29 | 通用电气公司 | Root sleeve for wind turbine blade |
CN103711655A (en) * | 2013-12-26 | 2014-04-09 | 中国科学院工程热物理研究所 | Large-thickness blunt-trailing-edge wind turbine blade |
CN103797242A (en) * | 2011-06-03 | 2014-05-14 | 叶片动力学有限公司 | A wind turbine rotor |
CN104929865A (en) * | 2010-10-22 | 2015-09-23 | 三菱重工业株式会社 | Wind turbine blade, wind power generation system including the same, and method for designing wind turbine blade |
CN106741857A (en) * | 2017-03-02 | 2017-05-31 | 南京那尔朴电子有限公司 | A kind of propeller that can be adjusted with thrust |
Families Citing this family (59)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2488151C (en) * | 2002-06-05 | 2009-04-28 | Aloys Wobben | Rotor blade for a wind power plant |
CN101194102B (en) | 2005-02-22 | 2012-04-25 | 维斯塔斯风力系统有限公司 | Wind turbine blade |
EP1845258A1 (en) | 2006-04-10 | 2007-10-17 | Siemens Aktiengesellschaft | Wind turbine rotor blade |
DE102006017897B4 (en) | 2006-04-13 | 2008-03-13 | Repower Systems Ag | Rotor blade of a wind turbine |
ES2294927B1 (en) * | 2006-05-31 | 2009-02-16 | Gamesa Eolica, S.A. | AIRLINER SHOVEL WITH DIVERGING OUTPUT EDGE. |
KR100926792B1 (en) * | 2006-12-29 | 2009-11-13 | 한국에너지기술연구원 | Tip airfoil of wind power generator for stall control and steady speed operation in low wind speed with improved contamination dullness |
US8197218B2 (en) * | 2007-11-08 | 2012-06-12 | Alliance For Sustainable Energy, Llc | Quiet airfoils for small and large wind turbines |
US20090148291A1 (en) * | 2007-12-06 | 2009-06-11 | General Electric Company | Multi-section wind turbine rotor blades and wind turbines incorporating same |
US20090148285A1 (en) * | 2007-12-06 | 2009-06-11 | General Electric Company | Multi-section wind turbine rotor blades and wind turbines incorporating same |
EP2078851A1 (en) | 2008-01-14 | 2009-07-15 | Lm Glasfiber A/S | Wind turbine blade and hub assembly |
DE102008026474A1 (en) | 2008-06-03 | 2009-12-10 | Mickeler, Siegfried, Prof. Dr.-Ing. | Rotor blade for a wind turbine and wind turbine |
AU2009292717B2 (en) | 2008-09-19 | 2014-10-23 | Wobben Properties Gmbh | Wind turbine with low induction tips |
WO2010043645A2 (en) * | 2008-10-14 | 2010-04-22 | Vestas Wind Systems A/S | Wind turbine blade with device for changing the aerodynamic surface or shape |
CA2741479A1 (en) * | 2008-10-22 | 2010-04-29 | Vec Industries, L.L.C. | Wind turbine blade and method for manufacturing thereof |
US7988421B2 (en) | 2009-03-31 | 2011-08-02 | General Electric Company | Retrofit sleeve for wind turbine blade |
DE102009002501A1 (en) | 2009-04-20 | 2010-10-28 | Wobben, Aloys | Rotor blade element and manufacturing process |
US8241000B2 (en) * | 2009-06-16 | 2012-08-14 | Heartland Energy Solutions, LLC. | Wind turbine rotor blade and airfoil section |
US8011886B2 (en) | 2009-06-30 | 2011-09-06 | General Electric Company | Method and apparatus for increasing lift on wind turbine blade |
US8197208B2 (en) * | 2009-12-16 | 2012-06-12 | Clear Path Energy, Llc | Floating underwater support structure |
US9270150B2 (en) | 2009-12-16 | 2016-02-23 | Clear Path Energy, Llc | Axial gap rotating electrical machine |
ES2856894T3 (en) * | 2010-07-16 | 2021-09-28 | Lm Wind Power As | Narrow shoulder wind turbine blade with relatively thick airfoils |
DE102010040596A1 (en) | 2010-09-10 | 2012-03-15 | Aloys Wobben | Removable rotor blade tip |
JP5479300B2 (en) * | 2010-10-22 | 2014-04-23 | 三菱重工業株式会社 | Wind turbine blade, wind power generator equipped with the wind turbine blade, and wind turbine blade design method |
DK2479423T3 (en) | 2011-01-24 | 2018-05-28 | Siemens Ag | Wind turbine rotor blade element |
JP5479388B2 (en) * | 2011-02-28 | 2014-04-23 | 三菱重工業株式会社 | Wind turbine blade and wind power generator equipped with the same |
WO2013054404A1 (en) * | 2011-10-12 | 2013-04-18 | 三菱重工業株式会社 | Wind turbine blade, wind power generation device provided with same, and design method for wind turbine blade |
DE102012209935A1 (en) * | 2011-12-08 | 2013-06-13 | Wobben Properties Gmbh | Rear box, rotor blade with rear box and wind turbine with such rotor blade |
US10060274B2 (en) | 2012-03-13 | 2018-08-28 | Corten Holding Bv | Twisted blade root |
NL2009286C2 (en) | 2012-08-06 | 2014-02-10 | Stichting Energie | Swallow tail airfoil. |
US11136958B2 (en) | 2012-08-06 | 2021-10-05 | Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek Tno | Swallow tail airfoil |
EP2713044B2 (en) * | 2012-09-28 | 2022-12-07 | Siemens Gamesa Renewable Energy A/S | Wind turbine rotor blade |
KR101331961B1 (en) | 2012-10-23 | 2013-11-22 | 한국에너지기술연구원 | Blade airfoil for wind turbine generator having trailing edge shape which possible inserting of aerodynamic control unit |
ITMI20121797A1 (en) | 2012-10-23 | 2014-04-24 | Wilic Sarl | AERODYNAMIC APPENDIX FOR A SHOVEL OF AN AEROGENERATOR AND SHOVEL OF AEROGENERATOR PROVIDED WITH THIS AERODYNAMIC APPENDIX |
CN103133273B (en) * | 2013-03-26 | 2015-12-02 | 国电联合动力技术有限公司 | A kind of thin airfoil type blade of large fan |
KR101466076B1 (en) * | 2013-08-22 | 2014-11-28 | 삼성중공업 주식회사 | Blade |
DE102013217128A1 (en) | 2013-08-28 | 2015-03-05 | Wobben Properties Gmbh | Rotor blade element for a wind energy plant, rotor blade, and a manufacturing method therefor and wind turbine with rotor blade |
EP3115599A4 (en) * | 2014-03-04 | 2017-03-29 | The Chugoku Electric Power Co., Inc. | Wind power generation device |
WO2015132884A1 (en) * | 2014-03-04 | 2015-09-11 | 中国電力株式会社 | Wind power generation device |
ITBZ20140002U1 (en) | 2014-03-13 | 2015-09-13 | Frassinelli Ernesto | WIND FOLDER WITH ADAPTIVE PROFILE ABLE TO MODIFY ITS STRUCTURE ON THE BASIS OF THE AERODYNAMIC PRESSURE THAT INVESTS IT, THE CLIMATE AND METEOROLOGICAL CHARACTERISTICS OF THE INSTALLATION SITE AND, COMPOSING A SINGLE ROTOR WITH ONE OR MORE ELEMENTS, WITH A MICRO-WIND GENERATOR WITH ROTATION AXIS PARALLEO AT THE AERODYNAMIC FLOW. |
USD801927S1 (en) * | 2014-09-15 | 2017-11-07 | II Raymond Cooper | Horizontal axis wind turbine with flow-through hub and nacelle and tandem blade configuration |
USD829172S1 (en) * | 2014-09-15 | 2018-09-25 | Raymond Cooper | Horizontal axis wind turbine with a flow-through hub, a nacelle, and a tandem blade configuration |
US11125205B2 (en) * | 2015-09-14 | 2021-09-21 | General Electric Company | Systems and methods for joining blade components of rotor blades |
DE102015116634A1 (en) * | 2015-10-01 | 2017-04-06 | Wobben Properties Gmbh | Wind turbine rotor blade and wind turbine |
DE102016213206A1 (en) | 2016-07-19 | 2018-01-25 | Wobben Properties Gmbh | Multilayer composite component |
DE102015220672A1 (en) | 2015-10-22 | 2017-04-27 | Wobben Properties Gmbh | Multilayer composite component |
CN105626373A (en) * | 2016-03-04 | 2016-06-01 | 云南电网有限责任公司电力科学研究院 | Rotary vane of wind turbine |
DE102016121554A1 (en) | 2016-11-10 | 2018-05-17 | Wobben Properties Gmbh | Multilayer composite component |
US11885297B2 (en) | 2017-05-10 | 2024-01-30 | Gerald L. Barber | Transitioning wind turbine |
US10788016B2 (en) | 2017-05-10 | 2020-09-29 | Gerald L. Barber | Transitioning wind turbine |
DE102017112742A1 (en) * | 2017-06-09 | 2018-12-13 | Wobben Properties Gmbh | Rotor blade for a wind turbine and wind turbine |
DE102017124861A1 (en) * | 2017-10-24 | 2019-04-25 | Wobben Properties Gmbh | Rotor blade of a wind turbine and method for its design |
WO2019217920A1 (en) | 2018-05-10 | 2019-11-14 | Joby Aero, Inc. | Electric tiltrotor aircraft |
US10710741B2 (en) | 2018-07-02 | 2020-07-14 | Joby Aero, Inc. | System and method for airspeed determination |
US11323214B2 (en) | 2018-09-17 | 2022-05-03 | Joby Aero, Inc. | Aircraft control system |
JP7401545B2 (en) | 2018-12-07 | 2023-12-19 | ジョビー エアロ インク | Rotor blades and their design methods |
US10960785B2 (en) | 2019-04-23 | 2021-03-30 | Joby Aero, Inc. | Battery thermal management system and method |
DE102019119027B4 (en) * | 2019-07-12 | 2022-04-28 | Wobben Properties Gmbh | Rotor blade and wind turbine |
CN112065651B (en) * | 2020-07-21 | 2021-12-14 | 兰州理工大学 | Airfoil for wind turbine blade layer of wind generating set |
DE102022104017A1 (en) | 2022-02-21 | 2023-08-24 | Wobben Properties Gmbh | Rotor blade of a wind turbine |
Family Cites Families (70)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1403069A (en) | 1921-08-12 | 1922-01-10 | Burne Edward Lancaster | Means for regulating the speed of wind motors |
US2622686A (en) | 1942-07-21 | 1952-12-23 | Chevreau Rene Louis Pier Marie | Wind motor |
US2428936A (en) | 1943-09-10 | 1947-10-14 | Goodrich Co B F | Aerodynamic brake |
US2485543A (en) * | 1943-10-19 | 1949-10-25 | Andreau Jean Edouard | Power plant |
US2465007A (en) * | 1944-01-05 | 1949-03-22 | Gen Motors Corp | Aircraft propeller |
US2400388A (en) | 1944-03-17 | 1946-05-14 | Goodrich Co B F | Aerodynamic brake |
US2442783A (en) | 1944-07-01 | 1948-06-08 | Us Sec War | Turbine rotor |
FR908631A (en) | 1944-08-01 | 1946-04-15 | Aero-engine improvements | |
US2453403A (en) | 1946-07-03 | 1948-11-09 | Charles E Bogardus | Windbreaker for parked aircraft |
US2616509A (en) | 1946-11-29 | 1952-11-04 | Thomas Wilfred | Pneumatic airfoil |
US2934150A (en) | 1955-12-21 | 1960-04-26 | United Aircraft Corp | Pressure-contoured spinner |
US3184187A (en) | 1963-05-10 | 1965-05-18 | Isaac Peter | Retractable airfoils and hydrofoils |
US3463420A (en) | 1968-02-28 | 1969-08-26 | North American Rockwell | Inflatable wing |
US3987984A (en) | 1973-04-09 | 1976-10-26 | Albert George Fischer | Semi-rigid aircraft wing |
US3874816A (en) | 1973-10-23 | 1975-04-01 | Thomas E Sweeney | Windmill blade |
FR2290585A1 (en) | 1974-11-07 | 1976-06-04 | Morin Bernard | Blade with variable profile for windmill rotor - has profile controlled by wind force and rotor speed |
SU577300A1 (en) | 1975-12-09 | 1977-10-25 | Свердловский Ордена Трудового Красного Знамени Горный Институт Им. В.В.Вахрушева | Turbine machine blade |
DE2829716A1 (en) | 1977-07-07 | 1979-01-25 | Univ Gakko Hojin Tokai | WIND POWER MACHINE WITH VERTICAL AXIS |
JPS5928754B2 (en) | 1979-05-18 | 1984-07-16 | 富治 高山 | Vertical axis wind turbine blade |
US4274011A (en) | 1980-03-14 | 1981-06-16 | Marvin Garfinkle | Wind turbine for marine propulsion |
US4408958A (en) | 1980-12-23 | 1983-10-11 | The Bendix Corporation | Wind turbine blade |
DE3113079C2 (en) | 1981-04-01 | 1985-11-21 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Large aerodynamic wing and process for its manufacture |
DE3126677A1 (en) | 1981-07-07 | 1983-01-20 | Erno-Raumfahrttechnik Gmbh, 2800 Bremen | Rotor blade design for high-speed rotors |
US4519746A (en) | 1981-07-24 | 1985-05-28 | United Technologies Corporation | Airfoil blade |
US4419053A (en) | 1981-11-20 | 1983-12-06 | Fairchild Swearingen Corporation | Propeller spinner |
US4498017A (en) | 1982-12-16 | 1985-02-05 | Parkins William E | Generating power from wind |
EP0181363A1 (en) | 1984-04-26 | 1986-05-21 | SIR HENRY LAWSON-TANCRED, SONS & COMPANY LTD. | Wind turbine blades |
US4699568A (en) | 1984-06-25 | 1987-10-13 | Hartzell Propeller Inc. | Aircraft propeller with improved spinner assembly |
US4613760A (en) | 1984-09-12 | 1986-09-23 | The English Electric Company Limited | Power generating equipment |
CH666728A5 (en) * | 1985-01-18 | 1988-08-15 | Escher Wyss Gmbh | ROTOR OF A WIND TURBINE. |
JPS61192864A (en) * | 1985-02-20 | 1986-08-27 | Yamaha Motor Co Ltd | Rotor blade structure of wind mill |
FR2587675A1 (en) | 1985-09-24 | 1987-03-27 | Dumortier Paul | Ailerons having self-deforming reversible profiles |
FR2590229B1 (en) | 1985-11-19 | 1988-01-29 | Onera (Off Nat Aerospatiale) | IMPROVEMENTS ON AIR PROPELLERS WITH REGARD TO THE PROFILE OF THEIR BLADES |
DE3875640D1 (en) | 1987-03-14 | 1992-12-10 | M T B Manoevriertechnisches Bu | FLOW BODY FLOWED BY AIR OR WATER. |
US4830574A (en) | 1988-02-29 | 1989-05-16 | United Technologies Corporation | Airfoiled blade |
SU1539378A1 (en) | 1988-03-29 | 1990-01-30 | Институт Электродинамики Ан Усср | Blade of wind motor |
US4976587A (en) * | 1988-07-20 | 1990-12-11 | Dwr Wind Technologies Inc. | Composite wind turbine rotor blade and method for making same |
GB8829836D0 (en) | 1988-12-21 | 1989-02-15 | British Aerospace | Wing flap hoot suppression |
GB2227286A (en) | 1989-01-17 | 1990-07-25 | Howden Wind Turbines Limited | Control of a wind turbine and adjustable blade therefor |
DE3913505A1 (en) | 1989-04-25 | 1989-11-16 | Astrid Holzem | WING WITH AERODYNAMIC BRAKE FOR WIND ENGINES |
DE4002972C2 (en) | 1990-02-01 | 1994-06-16 | Guenter Waldherr | Wing with changeable profile, especially for use as a sail |
JPH05189146A (en) | 1992-01-16 | 1993-07-30 | Hiroo Yasui | Track ball-mouse |
US5527151A (en) * | 1992-03-04 | 1996-06-18 | Northern Power Systems, Inc. | Advanced wind turbine with lift-destroying aileron for shutdown |
IL105107A (en) * | 1992-03-18 | 1996-06-18 | Advanced Wind Turbines Inc | Wind turbines |
US5320491A (en) | 1992-07-09 | 1994-06-14 | Northern Power Systems, Inc. | Wind turbine rotor aileron |
US5417548A (en) * | 1994-01-14 | 1995-05-23 | Midwest Research Institute | Root region airfoil for wind turbine |
US5562420A (en) | 1994-03-14 | 1996-10-08 | Midwest Research Institute | Airfoils for wind turbine |
DE4428731A1 (en) | 1994-08-15 | 1996-02-22 | Infan Gmbh Ingenieurgesellscha | Variable length rotor blade for wind power systems |
DE4435606A1 (en) | 1994-10-06 | 1996-04-11 | Manfred Dipl Ing Maibom | Size adjustable blade for wind power rotor |
US5570859A (en) | 1995-01-09 | 1996-11-05 | Quandt; Gene A. | Aerodynamic braking device |
US5570997A (en) | 1995-07-17 | 1996-11-05 | Pratt; Charles W. | Horizontal windmill with folding blades |
GB2311978A (en) | 1996-04-10 | 1997-10-15 | Robert Pyatt | Adjustable wing |
DE19719221C1 (en) | 1997-05-07 | 1998-10-29 | Roland Stelzer | Rotor blade for wind generator |
US6420795B1 (en) | 1998-08-08 | 2002-07-16 | Zond Energy Systems, Inc. | Variable speed wind turbine generator |
US6068446A (en) * | 1997-11-20 | 2000-05-30 | Midwest Research Institute | Airfoils for wind turbine |
US6015115A (en) | 1998-03-25 | 2000-01-18 | Lockheed Martin Corporation | Inflatable structures to control aircraft |
US6133716A (en) | 1998-10-23 | 2000-10-17 | Statordyne, Inc. | High-efficiency high-power uninterrupted power system |
ES2178903B1 (en) * | 1999-05-31 | 2004-03-16 | Torres Martinez M | SHOVEL FOR AEROGENERATOR. |
DE19962989B4 (en) * | 1999-12-24 | 2006-04-13 | Wobben, Aloys, Dipl.-Ing. | Rotor blade for wind turbines |
DE10003385A1 (en) * | 2000-01-26 | 2001-08-02 | Aloys Wobben | Wind turbine |
US6503058B1 (en) * | 2000-05-01 | 2003-01-07 | Zond Energy Systems, Inc. | Air foil configuration for wind turbine |
US6523781B2 (en) | 2000-08-30 | 2003-02-25 | Gary Dean Ragner | Axial-mode linear wind-turbine |
US6951443B1 (en) | 2000-09-08 | 2005-10-04 | General Electric Company | Wind turbine ring/shroud drive system |
US7204674B2 (en) | 2000-12-23 | 2007-04-17 | Aloys Wobben | Rotor blade for a wind power installation |
US6682302B2 (en) | 2001-03-20 | 2004-01-27 | James D. Noble | Turbine apparatus and method |
US6465902B1 (en) * | 2001-04-18 | 2002-10-15 | The United States Of America As Represented By The Secretary Of The Navy | Controllable camber windmill blades |
US7059833B2 (en) | 2001-11-26 | 2006-06-13 | Bonus Energy A/S | Method for improvement of the efficiency of a wind turbine rotor |
CA2488151C (en) * | 2002-06-05 | 2009-04-28 | Aloys Wobben | Rotor blade for a wind power plant |
DE10307682A1 (en) * | 2002-06-05 | 2004-01-08 | Aloys Wobben | Rotor blade of a wind turbine |
USD584686S1 (en) * | 2007-07-23 | 2009-01-13 | Aloys Wobben | Nacelle of a wind turbine |
-
2003
- 2003-04-28 DE DE10319246A patent/DE10319246A1/en not_active Withdrawn
-
2004
- 2004-03-29 PT PT47239884T patent/PT1620646T/en unknown
- 2004-03-29 EP EP04723988.4A patent/EP1620646B1/en active Active
- 2004-03-29 US US10/554,628 patent/US7946803B2/en active Active
- 2004-03-29 DK DK04723988.4T patent/DK1620646T3/en active
- 2004-03-29 EP EP10183781.3A patent/EP2258943A3/en not_active Withdrawn
- 2004-03-29 ES ES04723988T patent/ES2778830T3/en active Active
- 2004-03-29 AU AU2004234487A patent/AU2004234487B2/en not_active Ceased
- 2004-03-29 KR KR1020057020515A patent/KR100812796B1/en active IP Right Grant
- 2004-03-29 WO PCT/EP2004/003294 patent/WO2004097215A1/en active Application Filing
- 2004-03-29 CN CNB2004800114863A patent/CN100366893C/en not_active Expired - Fee Related
- 2004-03-29 NZ NZ543574A patent/NZ543574A/en unknown
- 2004-03-29 CA CA2524208A patent/CA2524208C/en not_active Expired - Fee Related
- 2004-03-29 JP JP2006504897A patent/JP4504971B2/en not_active Expired - Fee Related
- 2004-03-29 CA CA2683764A patent/CA2683764C/en not_active Expired - Fee Related
- 2004-03-29 BR BRPI0409782-3A patent/BRPI0409782B1/en active IP Right Grant
- 2004-04-28 AR ARP040101437A patent/AR046912A1/en not_active Application Discontinuation
-
2005
- 2005-10-14 ZA ZA200508323A patent/ZA200508323B/en unknown
- 2005-11-25 NO NO20055599A patent/NO20055599L/en not_active Application Discontinuation
-
2009
- 2009-10-23 JP JP2009244773A patent/JP5334796B2/en not_active Expired - Fee Related
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101749188B (en) * | 2008-12-03 | 2014-01-29 | 通用电气公司 | Root sleeve for wind turbine blade |
CN102192079A (en) * | 2010-03-18 | 2011-09-21 | 诺德克斯能源有限公司 | Wind turbine rotor blade |
CN102192109A (en) * | 2010-03-18 | 2011-09-21 | 诺德克斯能源有限公司 | Wind turbine rotor blade |
CN102407779A (en) * | 2010-09-21 | 2012-04-11 | 周鹏 | Power generation device for power motor vehicle |
CN102407779B (en) * | 2010-09-21 | 2014-10-01 | 周鹏 | Power generation device for power motor vehicle |
CN104929865A (en) * | 2010-10-22 | 2015-09-23 | 三菱重工业株式会社 | Wind turbine blade, wind power generation system including the same, and method for designing wind turbine blade |
CN102003333A (en) * | 2010-12-21 | 2011-04-06 | 中国科学院工程热物理研究所 | Wind turbine blade with de-noising function |
CN102003333B (en) * | 2010-12-21 | 2012-01-11 | 中国科学院工程热物理研究所 | Wind turbine blade with de-noising function |
CN103797242A (en) * | 2011-06-03 | 2014-05-14 | 叶片动力学有限公司 | A wind turbine rotor |
CN103797242B (en) * | 2011-06-03 | 2017-02-15 | 叶片动力学有限公司 | A wind turbine rotor |
US10125741B2 (en) | 2011-06-03 | 2018-11-13 | Blade Dynamics Limited | Wind turbine rotor |
CN103244359A (en) * | 2013-05-30 | 2013-08-14 | 国电联合动力技术有限公司 | Moderate-thickness airfoil blade of large-scale fan |
CN103321857A (en) * | 2013-07-08 | 2013-09-25 | 国电联合动力技术有限公司 | Large-thickness blunt-trailing-edge airfoil-shaped blade of large-scale wind turbine |
CN103711655A (en) * | 2013-12-26 | 2014-04-09 | 中国科学院工程热物理研究所 | Large-thickness blunt-trailing-edge wind turbine blade |
CN103711655B (en) * | 2013-12-26 | 2016-04-06 | 中国科学院工程热物理研究所 | The blunt trailing edge pneumatic equipment blades made of a kind of heavy thickness |
CN106741857A (en) * | 2017-03-02 | 2017-05-31 | 南京那尔朴电子有限公司 | A kind of propeller that can be adjusted with thrust |
Also Published As
Publication number | Publication date |
---|---|
AR046912A1 (en) | 2006-01-04 |
NO20055599L (en) | 2005-11-25 |
CA2683764A1 (en) | 2004-11-11 |
JP4504971B2 (en) | 2010-07-14 |
EP1620646A1 (en) | 2006-02-01 |
PT1620646T (en) | 2020-04-23 |
DE10319246A1 (en) | 2004-12-16 |
ES2778830T3 (en) | 2020-08-12 |
JP2006524772A (en) | 2006-11-02 |
CN100366893C (en) | 2008-02-06 |
JP5334796B2 (en) | 2013-11-06 |
WO2004097215A1 (en) | 2004-11-11 |
CA2683764C (en) | 2013-04-30 |
CA2524208A1 (en) | 2004-11-11 |
KR20060017761A (en) | 2006-02-27 |
KR100812796B1 (en) | 2008-03-12 |
ZA200508323B (en) | 2006-06-28 |
CA2524208C (en) | 2012-02-28 |
BRPI0409782B1 (en) | 2014-05-20 |
AU2004234487A1 (en) | 2004-11-11 |
NZ543574A (en) | 2009-02-28 |
EP1620646B1 (en) | 2020-01-22 |
EP2258943A3 (en) | 2013-10-02 |
JP2010043650A (en) | 2010-02-25 |
AU2004234487B2 (en) | 2009-02-19 |
BRPI0409782A (en) | 2006-05-30 |
DK1620646T3 (en) | 2020-04-14 |
EP2258943A2 (en) | 2010-12-08 |
US20070036657A1 (en) | 2007-02-15 |
US7946803B2 (en) | 2011-05-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1780982A (en) | Rotor blade of a wind energy facility | |
DK2341245T3 (en) | A device for increasing the buoyancy of the wind turbine blade | |
EP2647835B1 (en) | Flexible flap arrangement for a wind turbine rotor blade | |
EP2292926B1 (en) | Wind generator blade with hyper-supporting elements | |
US9523279B2 (en) | Rotor blade fence for a wind turbine | |
CN109113924B (en) | Wind turbine blade assembled from inboard and outboard portions having different types of load bearing structures | |
CN102758722B (en) | Wind turbine and wind turbine blade | |
EP2107235A1 (en) | A wind turbine blade with an auxiliary airfoil | |
US20100215494A1 (en) | Wind Turbine Rotor Blade | |
EP2309119A1 (en) | Windmill blade and wind power generator using same | |
US20100135806A1 (en) | Hinged wind turbine blade tips | |
CN1659376A (en) | Rotor blade for a wind power plant | |
WO2010133649A3 (en) | A wind turbine and a blade for a wind turbine | |
WO2009126312A2 (en) | Conical helicoid wind turbine | |
US8851857B2 (en) | Wind turbine blade and wind power generator using the same | |
EP2716907B1 (en) | Wind turbine blade and methods of operating it | |
CN105917116A (en) | Dual purpose slat-spoiler for wind turbine blade | |
JP5946812B2 (en) | Wind turbine rotor and wind power generator | |
EP3293392B1 (en) | Wind turbine blade comprising an edgewise stabilizer | |
WO2012095478A1 (en) | Wind turbine blade, wind turbine and method of controlling such | |
KR20150082981A (en) | a blade for wind generator, a generator including it and a method for improving aerodynamics characteristics and a control method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080206 |